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Published in 2020 at "AIAA Journal"
DOI: 10.2514/1.j059856
Abstract: Shock tunnel experiments are presented that examine combustion modes of ethylene and a 64/36% ethylene/methane mixture under Mach 8 flight-representative conditions within an axisymmetric scramjet ...
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Keywords:
combustion modes;
experimental scramjet;
mach flight;